JP2004520209A5 - - Google Patents

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Publication number
JP2004520209A5
JP2004520209A5 JP2001518316A JP2001518316A JP2004520209A5 JP 2004520209 A5 JP2004520209 A5 JP 2004520209A5 JP 2001518316 A JP2001518316 A JP 2001518316A JP 2001518316 A JP2001518316 A JP 2001518316A JP 2004520209 A5 JP2004520209 A5 JP 2004520209A5
Authority
JP
Japan
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2001518316A
Other languages
Japanese (ja)
Other versions
JP3998978B2 (en
JP2004520209A (en
Filing date
Publication date
Priority claimed from GBGB9919787.3A external-priority patent/GB9919787D0/en
Application filed filed Critical
Publication of JP2004520209A publication Critical patent/JP2004520209A/en
Publication of JP2004520209A5 publication Critical patent/JP2004520209A5/ja
Application granted granted Critical
Publication of JP3998978B2 publication Critical patent/JP3998978B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001518316A 1999-08-21 2000-08-16 Manufacturing and assembly of structures Expired - Fee Related JP3998978B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9919787.3A GB9919787D0 (en) 1999-08-21 1999-08-21 Manufacture and assembly of structures
PCT/GB2000/003165 WO2001014208A1 (en) 1999-08-21 2000-08-16 Manufacture and assembly of structures

Publications (3)

Publication Number Publication Date
JP2004520209A JP2004520209A (en) 2004-07-08
JP2004520209A5 true JP2004520209A5 (en) 2007-03-22
JP3998978B2 JP3998978B2 (en) 2007-10-31

Family

ID=10859545

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001518316A Expired - Fee Related JP3998978B2 (en) 1999-08-21 2000-08-16 Manufacturing and assembly of structures

Country Status (9)

Country Link
US (1) US6907651B1 (en)
EP (1) EP1204550B1 (en)
JP (1) JP3998978B2 (en)
AT (1) ATE241498T1 (en)
AU (1) AU6584900A (en)
DE (1) DE60003043T2 (en)
ES (1) ES2200909T3 (en)
GB (1) GB9919787D0 (en)
WO (1) WO2001014208A1 (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0126957D0 (en) * 2001-11-09 2002-01-02 Bae Systems Plc Manufacture and assembly of structures
GB0222288D0 (en) * 2002-09-25 2002-10-30 Airbus Uk Ltd Method and apparatus for joining aircraft components
US7487901B2 (en) * 2004-07-29 2009-02-10 The Boeing Company Friction stir welding of joints with shims
GB0519364D0 (en) * 2005-09-22 2005-11-02 Airbus Uk Ltd Assembly of aircraft components
GB0525690D0 (en) 2005-12-16 2006-01-25 Airbus Uk Ltd Assembly of aircraft components
FR2905739B1 (en) * 2006-09-08 2008-11-07 Airbus France Sas PANEL ASSEMBLY AND METHOD OF MOUNTING PANEL ASSEMBLY
JP4657194B2 (en) * 2006-11-20 2011-03-23 本田技研工業株式会社 Level adjustment structure for leading edge skin and method for assembling leading edge skin
US20090040247A1 (en) * 2007-08-07 2009-02-12 Mark Cato Micro shim for moving coil actuator
GB0720702D0 (en) * 2007-10-23 2007-12-05 Airbus Uk Ltd A shim for arrangement against a structural component and a method making a shim
US9381649B2 (en) 2012-06-25 2016-07-05 Systems Machine Automation Components Corporation Robotic finger
US9748824B2 (en) 2012-06-25 2017-08-29 Systems Machine Automation Components Corporation Linear actuator with moving central coil and permanent side magnets
US9731418B2 (en) 2008-01-25 2017-08-15 Systems Machine Automation Components Corporation Methods and apparatus for closed loop force control in a linear actuator
DE102008010197B4 (en) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Method for connecting two fuselage sections with the creation of a transverse joint and transverse joint connection
US9586367B2 (en) * 2008-11-04 2017-03-07 Lockheed Martin Corporation Composite laminate thickness compensation
RU2518927C2 (en) * 2009-10-08 2014-06-10 Мицубиси Хеви Индастрис, Лтд. Structure made of composite materials, aircraft main wing and body containing said structure
US9186849B2 (en) 2009-12-10 2015-11-17 Michael Spellman Composite part manufacturing compensation system and method
WO2012040620A2 (en) 2010-09-23 2012-03-29 Smac Inc Low cost multi-coil linear actuator
ES2396881B1 (en) * 2010-11-30 2014-01-29 Airbus Operations, S.L. INTERFACE PROVISION BETWEEN TWO COMPONENTS OF AN AIRCRAFT STRUCTURE USING A SEALING PIECE.
US9871435B2 (en) 2014-01-31 2018-01-16 Systems, Machines, Automation Components Corporation Direct drive motor for robotic finger
US10807248B2 (en) 2014-01-31 2020-10-20 Systems, Machines, Automation Components Corporation Direct drive brushless motor for robotic finger
US10429211B2 (en) 2015-07-10 2019-10-01 Systems, Machines, Automation Components Corporation Apparatus and methods for linear actuator with piston assembly having an integrated controller and encoder
EP3353558A1 (en) 2015-09-24 2018-08-01 Systems, Machines, Automation Components Corporation Magnetically-latched actuator
US10675723B1 (en) 2016-04-08 2020-06-09 Systems, Machines, Automation Components Corporation Methods and apparatus for inserting a threaded fastener using a linear rotary actuator
US10865085B1 (en) 2016-04-08 2020-12-15 Systems, Machines, Automation Components Corporation Methods and apparatus for applying a threaded cap using a linear rotary actuator
US10205355B2 (en) 2017-01-03 2019-02-12 Systems, Machines, Automation Components Corporation High-torque, low-current brushless motor
DE102017222897A1 (en) * 2017-12-15 2019-06-19 MTU Aero Engines AG Fiber composite component assembly, fiber composite component system, and method of making a fiber composite component system
CN115648636A (en) * 2022-09-28 2023-01-31 成都飞机工业(集团)有限责任公司 Composite material workpiece gluing method and device, storage medium and equipment

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3609116A (en) 1968-12-06 1971-09-28 Gen Dynamics Corp Moldable shim material for dimensional and aerodynamic surface control of aerospace structure
US4478915A (en) 1983-11-07 1984-10-23 United Technologies Corporation Corrosion resistant shim for electrically joining incompatible materials
US4861643A (en) * 1987-03-13 1989-08-29 The Boeing Company Aerospace structure having a cast-in-place noncompressible void filler
US5385050A (en) 1992-04-07 1995-01-31 Northrop Grumman Corporation Gap measurement for shim manufacture

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